Laserfiche WebLink
W. MICHAEL CARROLL, PE <br />COUNTY OF SAN JOAQUIN DEPARTMENT OF PUBLIC WORKS <br />DECEMBER 22, 2009 <br />failure within the GCL. The proposed construction specifications for Module 5 were sent to GSE, the <br />geosynthetics manufacturer for Module 4 liner system construction, to procure samples of geomembrane <br />and GCL for testing representative of the Module 5 specifications. The GCL specification included <br />minimum peel strength of 35 pounds measured according to American Society for Testing and Materials <br />(ASTM) D4632. The geomembrane specification included an asperity height of at least 20 mils <br />measured according to Geosynthetic Research Institute (GRI) GM12. Precision Geosynthetic <br />Laboratories (Precision) performed three sets of direct shear tests. Two were performed at normal <br />stresses of 5,000, 10,000, 15,000, and 20,000 psf with the GCL clamped so the failure plane was at the <br />geomembrane-CGL interface. The remaining set was performed at normal stresses of 15,000 and 20,000 <br />psf with the GCL floating to allow internal failure. Table 3 defines the general test conditions prescribed <br />for this round of interface testing with the exception that there was no required shear strength. <br />Detailed results of the testing are included in Attachment A. For the set with the GCL in a floating <br />configuration, Precision reported that failure occurred at the geomembrane-GCL interface for the test <br />point at 15,000 psf and internal to the GCL for the test point at 20,000 psf. However, after review and <br />discussion, we believe internal failure of the GCL occurred for both points. The reasons are the <br />reduction in large displacement shear strength from the tests with the GCL in a clamped configuration <br />and that the two large displacement shear strengths are essentially the same for the two normal stresses. <br />A multi -linear failure envelope, shown in Figure A, was developed using the large displacement shear <br />strengths from the tests performed by Precision, including the points representing internal GCL failure. <br />We believe this failure envelope is conservative because of the inclusion of the internal GCL failure <br />points and because the specifications for the future modules will be revised to require a higher internal <br />strength GCL. Also, the failure envelope does not include adhesion and was plotted through the origin. <br />This failure envelope was used as the liner shear strength in the slope stability analysis of the future <br />modules (5 through 11). <br />The static factors of safety for the permanent slopes Sections 4-4' and 5-5' using the liner failure <br />envelope defined in Figure A are > 1.5. Sections 44' and 5-5' are shown in Figures 6 and 7, <br />respectively. Results are summarized in Table 1. Detailed output is included in Attachment B. <br />The static FS for Section 3-3', the critical interim slope, was < 1.5. Since the interim slope configuration <br />may be repeated during facility development and may remain for a relatively long time (a few years), a <br />static FS of 1.5 was established as the stability criterion as discussed in Section 2.2.1 of Appendix E. A <br />200 feet setback was added to the interim slope at an elevation of 200 feet msl. The resulting slope <br />impinged on the south facing permanent slope meaning the interim slope with a toe at the north edge of <br />Module 9 is not the most critical. Section 3-3' was moved so the toe is at the north edge of Module 10 <br />and reanalyzed. The slope is still 3:1 with a 20 -feet wide bench every 50 vertical feet. The updated <br />Section 3-3' is shown in the revised Figure 5, and the revised location is shown in Figures 1 and 2. The <br />resulting static FS is 1.65. Results are summarized in Table 1. Detailed output is included in Attachment <br />B. The 200 -feet wide setback at an elevation of 200 feet msl will be designed into the operations plan so <br />all internal interim slopes will include the setback at el. 200 feet msl. <br />We will modify the GCI. specifications for all future modules to attempt to avoid internal GCL failure. <br />This should increase actual liner interface strengths in the future modules. We plan to do this by <br />specifying a higher GCL peel strength. We believe a minimum GCL peel strength of at least 10 pounds <br />PAGE 5 <br />